Pressure panels

US9199713B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9199713-B2
Application numberUS-201313936468-A
CountryUS
Kind codeB2
Filing dateJul 8, 2013
Priority dateJul 8, 2013
Publication dateDec 1, 2015
Grant dateDec 1, 2015

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

Anisotropic pressure panels are disclosed. The pressure panels include at least two distinct regions, with one region yielding to lateral deformation more than at least one other region. The regions each independently may include a plurality of beads, such beads optionally integrally formed in the body of the pressure panel. In aerospace applications, the pressure panel may be coupled to load-bearing structures, such as wings, and may at least partially define a wheel well.

First claim

Opening claim text (preview).

The invention claimed is: 1. An aircraft, comprising: a fuselage with a pressurized compartment; a wing assembly including outboard wing sections and a wing center section between the outboard wing sections; and at least one pressure panel including: a body having a width defining a lateral direction, a length defining a longitudinal direction, and a thickness that is substantially less than the width and the length, wherein the body is a monolithic body; wherein the body h…

Assignees

Inventors

Classifications

  • Cross-Sectional Technologies · mapped topic

  • B64C1/06Primary

    Operations & Transport · mapped topic

  • Cross-Sectional Technologies · mapped topic

  • Operations & Transport · mapped topic

  • Cross-Sectional Technologies · mapped topic

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Frequently asked questions

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What does patent US9199713B2 cover?
Anisotropic pressure panels are disclosed. The pressure panels include at least two distinct regions, with one region yielding to lateral deformation more than at least one other region. The regions each independently may include a plurality of beads, such beads optionally integrally formed in the body of the pressure panel. In aerospace applications, the pressure panel may be coupled to load-b…
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification B64C1/06. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 01 2015 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).